An initiator assembly that includes a header body, a frame member, a plurality of terminals, an initiator chip, a plurality of contacts, and a support member. The frame member is coupled to the header body and defines an interior aperture. The terminals are received through the header body and the frame member. The initiator chip is received in the frame member and has a plurality of lands, a conductive bridge and a flyer that is disposed over the conductive bridge. Each of the contacts is soldered to an associated one of the terminals and an associated one of the lands. The support member is formed of plastic and encapsulates the frame member, the plurality of contacts, and a portion of the initiator chip. The support member forms a barrel aperture over the flyer. The input charge is formed of a secondary explosive and is disposed in-line with the barrel aperture.
|
20. An initiator assembly comprising:
a header body;
a frame member coupled to the header body, the frame member defining an interior aperture;
a plurality of terminals received through the header body and the frame member;
an initiator chip received in the interior aperture of the frame member, the initiator chip having a plurality of lands, a conductive bridge and a flyer disposed over the conductive bridge;
a plurality of contacts, each of the contacts being soldered to an associated one of the terminals and an associated one of the lands; and
a support member formed of plastic and encapsulating the frame member, the plurality of contacts, and a portion of the initiator chip, the support member forming a barrel aperture over the flyer; and
an input charge formed of a secondary explosive disposed in-line with the barrel aperture.
1. An initiator assembly comprising:
an input charge formed of a secondary explosive; and
a header assembly having a header body, a plurality of terminals, a plurality of seal members, an insulating spacer, a frame member, an initiator chip and a support member, the header body having an interior surface and a plurality of terminal apertures, each of the seal members being received in an associated one of the terminal apertures and being sealingly engaged to the header body and an associated one of the terminals, the insulating spacer being abutted against the interior surface of the header body, the frame member overlying the insulating spacer and defining an interior aperture, the initiator chip being received in the interior aperture in the frame member and having a plurality of bridge lands, a bridge and a flyer, each of the bridge lands being electrically coupled to an associated one of the terminals, the flyer being disposed on a side of the bridge opposite the header body such that the bridge is disposed along an initiation axis between the flyer and the header body, the support member overlying a portion of the initiator chip and defining a first header surface with a central aperture formed therethrough, wherein one of the initiator chip and the support member comprises a barrel, the barrel defining a barrel aperture that is disposed in-line with the flyer and the bridge along the initiation axis, and wherein the first header surface has a flatness that is less than or equal to 0.006 inch.
2. The initiator assembly of
3. The initiator assembly of
4. The initiator assembly of
5. The initiator assembly of
6. The initiator assembly of
7. The initiator assembly of
8. The initiator assembly of
9. The initiator assembly of
10. The initiator assembly of
12. The initiator assembly of
13. The initiator assembly of
14. The initiator assembly of
16. The initiator assembly of
17. The initiator assembly of
18. The initiator assembly of
19. The initiator assembly of
|
The present disclosure relates to an initiator assembly that is resistant to shock.
This section provides background information related to the present disclosure which is not necessarily prior art.
U.S. Pat. No. 7,571,679 discloses an energetic material initiation device with a header assembly that includes an exploding foil initiator. While this device works very well for its intended purpose, we have noted that in high-shock situations (i.e., where the device experiences high levels of shock before the device is operated) it is possible for the shock to crack the (compacted) input charge. The cracking of the input charge increases the risk that the input charge would fail to detonate.
We surmise that due to changes in elevation across the header assembly that are related to the thickness of the contacts, the thickness of the solder that is employed to secure the contacts to the exploding foil initiator, the thickness of the barrel, etc., the input charge is not supported to a maximum extent on a side adjacent the exploding foil initiator. Consequently, the void space between the header assembly and the input charge provides space for portions of the input charge to move by a sufficient amount in a high-shock situation to cause the input charge to crack.
This section provides a general summary of the disclosure, and is not a comprehensive disclosure of its full scope or all of its features.
In one form, the present disclosure provides an initiator assembly that includes an input charge formed of a secondary explosive and a header assembly having a header body, a plurality of terminals, a plurality of seal members, an insulating spacer, a frame member, an initiator chip and a support member. The header body has an interior surface and a plurality of terminal apertures. Each of the seal members is received in an associated one of the terminal apertures and is sealingly engaged to the header body and an associated one of the terminals. The insulating spacer is abutted against the interior surface of the header body. The frame member overlies the insulating spacer and defines an interior aperture. The initiator chip has a plurality of bridge lands, a bridge and a flyer. Each of the bridge lands is electrically coupled to an associated one of the terminals. The flyer is disposed on a side of the bridge opposite the header body such that the bridge is disposed along an initiation axis between the flyer and the header body. The support member overlies a portion of the initiator chip and defines an annular upper header surface with a central aperture formed therethrough. One of the initiator chip and the support member forms a barrel with a barrel aperture that is disposed in-line with the flyer and the bridge along the initiation axis. The annular upper header surface has a flatness that is less than or equal to 0.006 inch.
In still another form, the present disclosure provides an initiator assembly that includes a header body, a frame member, a plurality of terminals, an initiator chip, a plurality of contacts, and a support member. The frame member is coupled to the header body and defines an interior aperture. The terminals are received through the header body and the frame member. The initiator chip is received in the frame member and has a plurality of lands, a conductive bridge and a flyer that is disposed over the conductive bridge. Each of the contacts is soldered to an associated one of the terminals and an associated one of the lands. The support member is formed of plastic and encapsulates the frame member, the plurality of contacts, and a portion of the initiator chip. The support member forms a barrel aperture over the flyer. The input charge is formed of a secondary explosive and is disposed in-line with the barrel aperture.
Further areas of applicability will become apparent from the description provided herein. The description and specific examples in this summary are intended for purposes of illustration only and are not intended to limit the scope of the present disclosure.
The drawings described herein are for illustrative purposes only of selected embodiments and not all possible implementations, and are not intended to limit the scope of the present disclosure.
Corresponding reference numerals indicate corresponding parts throughout the several views of the drawings.
With reference to
With reference to
With reference to
The header body 40 can define first and second end faces 50 and 52, respectively, a shoulder 54, an annular shoulder wall 56, a plurality of terminal apertures 58 and an outer circumferentially extending surface 60. The shoulder 54 can be generally parallel to the first and second end faces 50 and 52 and can abut the annular shoulder wall 56. The shoulder wall 56 and the outer circumferentially extending surface 60 can be concentric with one another and can be disposed generally perpendicular to the shoulder 54. The terminal apertures 58 can be formed through the header body 40 generally perpendicular to the first and second end faces 50 and 52.
The terminals 42 can be received in respective ones of the terminal apertures 58 and can extend outwardly from the first and second end faces 50 and 52. It will be appreciated that the terminals 42 can be arranged in a non-symmetrical manner to thereby key the header 20 in a particular orientation relative to a fireset device (not shown) to which the initiator assembly 10 is to be coupled. It will also be appreciated that a keying feature, such as a tab (not shown) or a recess (not shown), can be incorporated into a portion of the header 20 (e.g., the header body 40) to key the header 20 in a particular orientation.
The seal members 44 can be formed of a suitable material, such as glass conforming to 2304 Natural or another dielectric material, and can be received into an associated one of the terminal apertures 58. The seal members 44 can sealingly engage the header body 40 as well as an associated one of the terminals 42.
The insulating spacer 22 can be formed of a suitable dielectric material, such as polycarbonate, synthetic resin bonded paper (SRBP) or epoxy resin bonded glass fabric (ERBGF), and can have a plurality of clearance apertures 68 that are sized to receive the terminals 42 therethrough. The insulating spacer 22 can be received onto the second end face 52 and within an area that is defined by the size (i.e., perimeter) of the annular shoulder wall 56.
With reference to
With reference to
Each of the contacts 28 can be formed of a suitable electrically conductive material, such as KOVAR®, and can electrically couple an associated one of the terminals 42 to an associated one of the bridge lands 82 and 84. In the example provided, each of the contacts 28 is soldered to an associated one of the terminals 42 and an associated one of the bridge lands 82 and 84. While the contacts 28 and the layer of solder between the contacts 28 and the bridge lands 82 and 84 can be relatively small, their presence significantly affects the overall flatness across the side of the initiator chip 26 that faces away from the second end face 52 (
With reference to
If desired, the support member 30 can be pre-formed and assembled to the initiator chip 26, the contacts 28 and the header body 40. In such case, it may be beneficial to have a substance, such as an epoxy adhesive, that is disposed between the support member 30 and the initiator chip 26 and the contacts 28 to secure the support member 30 to the initiator chip 26 and the contacts 28 and/or to fill void spaces that might otherwise be present between an interior surface 110 of the support member 30 and surfaces of the initiator chip 26 and the contacts 28. In the present example, the support member 30 is formed via injection molding directly onto the remainder of the header assembly 12 (i.e., the portion of the header assembly 12 that excludes the support member 30) so that no void spaces are present between the support member 30 and the initiator chip 26 and the support member 30 can be cohesively bonded to the initiator chip 26, the contacts 28, the frame member 24 and the second end surface 52 of the header body 40. Configuration in this manner encapsulates the insulating spacer 22, the frame member 24, the ends of the terminals 42 that are received through the seal members 44, the initiator chip 26 and the contacts 28, which can improve the overall rigidity of the header assembly 12. Molding of the support member 30 directly onto the remainder of the header assembly 12 also permits the barrel aperture (i.e., the through-bore 100 in the example provided) to be formed with a fillet radius 120 on a side of the barrel 108 that faces away from the bridge 86. Suitable materials from which the support member 30 may be formed via molding include polycarbonate, including optically transparent polycarbonates, and liquid-crystal polymer (LCP).
With reference to
Returning to
The input charge 16 can be received in the cavity 130 and can have an axial end 150 that can be abutted directly against the annular upper header surface 90. Optionally, as shown in
Returning to
The foregoing description of the embodiments has been provided for purposes of illustration and description. It is not intended to be exhaustive or to limit the disclosure. Individual elements or features of a particular embodiment are generally not limited to that particular embodiment, but, where applicable, are interchangeable and can be used in a selected embodiment, even if not specifically shown or described. The same may also be varied in many ways. Such variations are not to be regarded as a departure from the disclosure, and all such modifications are intended to be included within the scope of the disclosure.
Morales, Emmanuel, Nance, Christopher J., Meadows, Michael B.
Patent | Priority | Assignee | Title |
10935352, | Feb 04 2019 | Reynolds Systems, Inc. | Initiation system having plastic housing, which encapsulates an initiator, and a lid that hermetically seals the housing |
11009319, | Apr 18 2017 | Reynolds Systems, Inc. | Initiator assembly that is resistant to shock |
11448487, | Aug 19 2020 | Reynolds Systems, Inc. | Vibration resistant initiator assembly having exploding foil initiator |
11644286, | Aug 19 2020 | Reynolds Systems, Inc. | Vibration resistant initiator assembly having exploding foil initiator |
Patent | Priority | Assignee | Title |
6851370, | Apr 30 2002 | L-3 Communications Corporation | Integrated planar switch for a munition |
6923122, | Dec 10 2002 | REYNOLDS SYSTEMS, INC | Energetic material initiation device utilizing exploding foil initiated ignition system with secondary explosive material |
7430963, | Nov 29 2005 | REYNOLDS SYSTEMS, INC | Energetic material initiation device utilizing exploding foil initiated ignition system with secondary explosive material |
7543532, | May 09 2006 | Reynolds Systems, Inc. | Full function initiator with integrated planar switch |
7571679, | Sep 29 2006 | REYNOLDS SYSTEMS, INC | Energetic material initiation device having integrated low-energy exploding foil initiator header |
7661362, | Nov 29 2005 | Reynolds Systems, Inc. | Energetic material initiation device utilizing exploding foil initiated ignition system with secondary explosive material |
7690303, | Apr 22 2004 | Reynolds Systems, Inc.; REYNOLDS SYSTEMS, INC | Plastic encapsulated energetic material initiation device |
7866264, | Sep 29 2006 | Reynolds Systems, Inc. | Energetic material initiation device |
8100043, | Mar 28 2008 | ORBITAL ATK, INC | Detonator cartridge and methods of use |
8113117, | Sep 29 2006 | Reynolds Systems, Inc. | Energetic material initiation device |
8276516, | Oct 30 2008 | REYNOLDS SYSTEMS, INC | Apparatus for detonating a triaminotrinitrobenzene charge |
8408131, | Sep 29 2006 | Reynolds Systems, Inc.; REYNOLDS SYSTEMS, INC | Energetic material initiation device |
8485097, | Jun 11 2010 | Reynolds Systems, Inc.; REYNOLDS SYSTEMS INC | Energetic material initiation device |
8573122, | May 09 2006 | Reynolds Systems, Inc. | Full function initiator with integrated planar switch |
8701557, | Feb 07 2011 | Raytheon Company | Shock hardened initiator and initiator assembly |
8726808, | Dec 17 2010 | Reynolds Systems, Inc.; REYNOLDS SYSTEMS, INC | Initiator assembly having low-energy exploding foil initiator header and cover with axially threaded portion |
9038538, | Feb 28 2012 | Reynolds Systems, Inc.; REYNOLDS SYSTEMS, INC | Initiator assembly with gas and/or fragment containment capabilities |
9500448, | Jun 09 2015 | Reynolds Systems, Inc. | Bursting switch |
9816790, | Feb 07 2011 | Raytheon Company | Shock hardened initiator and initiator assembly |
9879951, | Feb 07 2011 | Raytheon Company | Shock hardened initiator and initiator assembly |
20170045342, | |||
DE102014010179, |
Executed on | Assignor | Assignee | Conveyance | Frame | Reel | Doc |
Apr 18 2017 | Reynolds Systems, Inc. | (assignment on the face of the patent) | / | |||
Apr 18 2017 | MORALES, EMMANUEL | REYNOLDS SYSTEMS, INC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 042045 | /0377 | |
Apr 18 2017 | MEADOWS, MICHAEL B | REYNOLDS SYSTEMS, INC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 042045 | /0377 | |
Apr 18 2017 | NANCE, CHRISTOPHER J | REYNOLDS SYSTEMS, INC | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 042045 | /0377 |
Date | Maintenance Fee Events |
Aug 26 2022 | M2551: Payment of Maintenance Fee, 4th Yr, Small Entity. |
Date | Maintenance Schedule |
Apr 23 2022 | 4 years fee payment window open |
Oct 23 2022 | 6 months grace period start (w surcharge) |
Apr 23 2023 | patent expiry (for year 4) |
Apr 23 2025 | 2 years to revive unintentionally abandoned end. (for year 4) |
Apr 23 2026 | 8 years fee payment window open |
Oct 23 2026 | 6 months grace period start (w surcharge) |
Apr 23 2027 | patent expiry (for year 8) |
Apr 23 2029 | 2 years to revive unintentionally abandoned end. (for year 8) |
Apr 23 2030 | 12 years fee payment window open |
Oct 23 2030 | 6 months grace period start (w surcharge) |
Apr 23 2031 | patent expiry (for year 12) |
Apr 23 2033 | 2 years to revive unintentionally abandoned end. (for year 12) |